Fairchild SA227-AC

Service difficulty reports · 2,182

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'SA227AC'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR MALA964961Rib · chafedDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WApr 13, 1996 · N60NE · Swrngn SA227AC · Trailing Edge FlapsSDR 96ZZZM928Hinge Arm · damagedDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WApr 13, 1996 · N60NE · Swrngn SA227AC · Trailing Edge FlapsSDR 96ZZZM927Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WIApr 13, 1996 · N60NE · Swrngn SA227AC · Trailing Edge FlapsSDR 96ZZZM876Hinge Arm · bentDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WIApr 13, 1996 · N60NE · Swrngn SA227AC · Trailing Edge FlapsSDR 96ZZZM875Rib · chafedDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WIApr 13, 1996 · N60NE · Swrngn SA227AC · Trailing Edge FlapsSDR MALA964949Fire Detector · malfunctionedFLT NR 3302 - DURING THE TAKEOFF ROLL IN MSP, THE LEFT ENGINE FIRE LIGHT ILLUMINATED. THE TAKEOFF ATTEMPT WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MX TESTED THE ENGINE WIRING. ALL CHECKS GOOD. Apr 12, 1996 · N425MA · Swrngn SA227AC · Fire DetectionSDR MALA964946Skin · dentedDURING AN INSPECTION IN MSP, FOUND FUSELAGE SKIN DENTED AFT OF CARGO DOOR BETWEEN FS 512 AND FS 530.810, JUST BELOW WL 75. DENTED AREA DIMENSIONS 8 INCHES BY .375 INCHES. FABRICATED A REPAIR DOUBLER (13 INCHES BY 5.25 INCHES ) AND INSTALLED IAW FAIRCHILD SRMApr 12, 1996 · N421MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA964945Door Frame · crackedMSP - DURING AN INSPECTION, FOUND AN APPROXIMATE .575 INCH CRACK IN THE CARGO DOOR FRAME PN 27-22085 AT FS 438.060. REPAIRED DAMAGE BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 INCH BY 1.825 INCH), FABRICATING, TREATING, AND INSTALLING A REPAIR ANGLE, REPAApr 12, 1996 · N421MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964965Skin · dentedDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND DENT DAMAGE TO LOWER FUSELAGE SKIN JUST AFT OF FS 493.247 AND ON BOTH LEFT AND RIGHT SIDE OF BL 0. COMBINED AREA OF DENT DAMAGE IS APPROX 14 INCHES BY 9 INCHES. DETEMINED THAT A SURFACE REPAIR DOUBLER Apr 11, 1996 · N60NE · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA964964Skin · damagedDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED AFT CARGO DOOR SKIN AT FORWARD AND AFT HINGE CUT OUTS, SKIN CHAFED ADN DAMAGED. COMPLETED REPAIRS BY REMOVING CHAFED AREAS AND INSTALLING REPAIR PATCHES IAW FAC ARP 52-30-9130 DATED 20 JUNE 1991. (M)Apr 11, 1996 · N60NE · Swrngn SA227AC · Cargo/Baggage DoorsSDR MALA964948Bus Light · flickersYNG - FLT 3367 - ON APPROACH THE RIGHT NON-ESSENTIAL BUS LIGHTS BEGAN TO FLICKER AND THE CREW NOTED AN ELECTRICAL SMELL. MAINTENANCE DEFERRED THE SYSTEM PER MEL 33-1C. (X)Apr 11, 1996 · N428MA · Swrngn SA227AC · DC Indicating SystemSDR MALA964947Brake · wornFLT 3089 - WHILE TAXIING IN DTW, THE CREW NOTED THAT THE RIGHT BRAKE WOULDN'T HOLD PRESSURE. MX REPLACED THE RIGHT INBOARD AND OUTBOARD BRAKE ASSEMBLIES. ALL CHECKS GOOD. (M)Apr 10, 1996 · N446MA · Swrngn SA227AC · Landing Gear Brake SystemSDR MALA964943Switch · lack of lubeYXU - FLT 3345 - ON CLIMB-OUT, THE RIGHT MAIN GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. ALL OTHER GEAR INDICATIONS NORMAL. THE AIRCRAFT CONTINUE TO DTW. MAINTENANCE CLEARED AND LUBED THE RIGHT LANDING GEAR SWITCHES. ALL CHECKS SATISFAApr 9, 1996 · N2692P · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964944Skin · dentedMSP - DURING AN INSPECTION, FOUND FUSELAGE SKIN DENTED AFT OF CARGO DOOR AT FS 493.00 AND WL 75.00. REMOVED DAMAGED AREA (8.00 INCHES BY 9.75 INCHES), FABRICATED REPAIR DOUBLER, REPAIR FILLER, AND INSTALLED IAW FAIRCHILD SRM 53-90-20, PAGES 64-65. (X)Apr 6, 1996 · N426MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR QXEA9600141Air Distr · odorNUMBER TWO BLEED AIR HAS NOXIOUS ODOR. INSPECTED AND PLACED ON MEL 21-4.Apr 5, 1996 · N385PH · Swrngn SA227AC · Air Distribution SystemSDR MALA964940Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK IN THE FUSELAGE FORWARD CARGO DOOR FRAME (PN 27-22085) AT FS 438. REPAIRS WERE COMPLETED BY REMOVING THE CRACKED AREA AND INSTALLING REPAIR DOUBLERS IAW FAC ARP 53-20-5503. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964939Intercostal · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT LOWER FUSELAGE INTERCOSTAL, AT FS 212.37 (PN 27-22104), CRACKED IN THE FLANGE RELIEF RADIUS. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER AND STIFFENER IAW FAApr 1, 1996 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964938Corner · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LOWER AFT PASSENGER DOOR CORNER, PN 27-24044, CRACKED AT SNUBBER ATTACH NUTPLATE. REPAIRS WERE COMPLETED BY REPLACING THE CORNER IAW FAC SRM'S 51-00-00, 51-30-02, 51-30-04, AND 51-40-00. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964937Skin · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER SKIN EDGE CRACKED OFF AT THE FORWARD HINGE RECESS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 52-10-8701, SRM 51-30-04 AND SRM 51-40-01. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964936Skin · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER SKIN EDGE CRACKED OFF AT THE AFT HINGE RECESS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 52-10-8701, SRM 51-30-04, AND SRM 51-40-01. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964935Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT INBOARD LOWER WING TO NACELLE TRANSIT/ATTACH ANGLE CRACKED APPROXIMATELY .750 INCHES AT THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 51-00-00 AND ARP 54-20-Apr 1, 1996 · N159MC · Swrngn SA227AC · Wing Miscellaneous StructureSDR MALA964934Sill Frame · crackedMSP - DURING A SCHEDULED INSPECTION, THE CARGO DOOR SILL FRAME AT FS 438 WAS FOUND TO HAVE A .25 INCH CRACK. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK, ENLARGING THE CUT OUT IN THE SILL, AND WET INSTALLING TWO DOUBLERS IAW FAC ARP 53-30-5507. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MEJA960303Engine · failedDURING LEVEL FLIGHT, THE RT ENGINE BEGAIN TO VIBRATE, THE ONLY ENGINE INDICATION WAS A 20 PERCENT LOSS OF TORQUE AND ALL OTHER INDICATIONS WERE NORMAL. AFTER ABOUT 15 SECONDS THE OIL PRESSURE GAUGE FLICKERED ONCE AND THE PILOTS SECURED THE ENGINE. THERE WAS Mar 29, 1996 · N340AE · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR MALA964933Frame · crackedMSP - DURING SCHEDULED MAINTENANCE, MAINTENANCE FOUND THE FUSELAGE FRAME AT FS 51.31 CRACKED AT THE RIGHT BAGGAGE DOOR LOWER LATCH RECEPTACLE CUT OUT. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING AN INTERNAL DOUBLER IAW FAC LAR 96-MALA-057Mar 28, 1996 · N426MA · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964930Switch · failedSTC - FLT 3494 - ON CLIMB-OUT, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. THE LIGHT ALSO FAILED TO ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN ON APPROACH TO MSP. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE LEFT Mar 28, 1996 · N439MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964929Switch · failedMSP - FLT 3082 - ON APPROACH, THE NOSE GEAR RED INTRANSIT LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION. ALL OTHER GEAR INDICATIONS WERE NORMAL. MAINTENANCE REPLACED BOTH NOSE LANDING GEAR DOWN POSITION SWITCHES. SYSTEM OPERATED SATISFACTORILY. (X)Mar 26, 1996 · N158MC · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964927Door Seal · looseFLT NR 3487 - AFTER DEPARTURE FROM YQT, THE CREW NOTED A FLAPPING NOISE FROM THE PASSENGER DOOR AREA. THE AIRCRAFT RETURNED TO YQT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SECURED A SHIM FOR THE PASSENGER DOOR SEAL. ALL SYSTEMS OPERATED SATISFACTOMar 23, 1996 · N26863 · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964928Uplock Switch · failedFLT NR 3353 - AFTER DEPARTURE FROM DTW, THE CREW NOTED THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NOSE GEAR UPLIMIT SWITCH. ALL SYSTEMar 22, 1996 · N60NE · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA964926Switch · failedFLIGHT NR 3078 - INBOUND TO MSP, THE CREW NOTED THE LEFT MAIN GEAR INTRANSIT LIGHT WAS INTERMITTENT. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT MAIN GEAR UP POSITION SWITCH. ALL SYSTEMS OPERATED SATISFMar 21, 1996 · N446MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964925Rib · crackDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT FLAP OUTBOARD END NOSE RIB. THEY REPLACED THE OUTBOARD END NOSE RIB IAW FAC SRM 57-90-60. (M)Mar 14, 1996 · N438MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA964924Skin · dentedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A DENT IN THE FUSELAGE SKIN AFT OF FS 493. THEY REPAIRED THE DENT BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Mar 14, 1996 · N438MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA964923Skin · dentedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A DENT IN THE FUSELAGE SKIN AFT OF FS 512. THEY REPAIRED THE DENT BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Mar 14, 1996 · N438MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA964921Cargo Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED CRACKS IN THE FORWARD CARGO DOOR FRAME GAS STRUT MOUNT HOLE. THEY REMOVED THE CRACKED PORTION AND FABRICATED AND INSTALLED A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARP 53-20-9503. (M)Mar 14, 1996 · N438MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964920Skin · damagedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED DAMAGE TO THE OUTER FUSELAGE SKIN AT THE PASSENGER DOOR FORWARD CORNER. THEY REPAIRED THE DAMAGE BY INSTALLING A DOUBLER IAW FAC LAR 96-MALA-042. (M)Mar 14, 1996 · N438MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA964919Torque Tube · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED WEAR ON THE RIGHT ELEVATOR TORQUE TUBE. THEY REPLACED THE TORQUE TUBE IAW FAC MM 27-30-00. (M)Mar 14, 1996 · N438MA · Swrngn SA227AC · Rudder Control SystemSDR AU960465Switch · faulty(AUS) LH ENGINE BEGAN TO ROTATE RAPIDLY WHEN AIRCRAFT BATTERY SWITCHES SELECTED ON - SUSPECT INTERNAL SHORT ACROSS THE STARTER SWITCH CONTACTS CAUSED CONTACTS TO STICKMar 14, 1996 · Swrngn SA227AC · Engine CrankingSDR COMA9620005Torque Tube · bentRUDDER PEDALS ARE OFFSET IN FLIGHT. FOUND RUDDER TORQUE TUBE BENT. REPLACED TORQUE TUBE.Mar 13, 1996 · N703CA · Swrngn SA227AC · Rudder Control SystemSDR MALA964917Selector · failedABR - FLT 3203 - ON CLIMB-OUT, LANDING GEAR LEVER LOCK OVERRIDE WAS REQUIRED TO RETRACT THE GEAR. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR. SYSTEM OPERATED SATISFACTORILY. (X)Mar 12, 1996 · N26863 · Swrngn SA227AC · Landing Gear SelectorSDR MALA964915Corner · puncturedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR AFT LOWER CORNER PUNCTURED. REPAIRS WERE COMPLETED BY REPLACING THE LOWER AFT CORNER, PN 27-24051-003, IAW FAC SRM 51-00-00, SRM 51-30-03, AND SRM 51-40-01. (X)Mar 12, 1996 · N26863 · Swrngn SA227AC · Cargo/Baggage DoorsSDR MALA964914Emergency Pin · out of positionMSP - FLT 3002 - ON CLIMB-OUT FROM MSP, LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPOSITIONED THE EMERGENCY PIN IN THE EMERGENCY GEAR SELECTOR TO THE NORMAL POSITION. SYSTEM OPERATED SATISFACTORILY. (X)Mar 12, 1996 · N446MA · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR 96ZZZX1371Spar · crackedDURING DISASSEMBLY OF AILERON TO REPLACE CRACKED AILERON SKINS, SPAR FOUND TO HAVE 3 CRACKS. THERE ARE TWO, 1.5 INCH CRACKS IN AREA OF OUTBOARD HINGE FITTING ATTACH HOLES AND ONE, .5 INCH CRACK IN AREA OF CENTER HINGE FITTING ATTACH HOLE. CRACKS ARE SUSPECTEMar 11, 1996 · N361AE · Swrngn SA227AC · AileronsSDR QXEA9600100O-Ring · cutMWH - NR 2 ENGINE SHUTDOWN IN-FLIGHT DUE TO LOW OIL PRESSURE INDICATION. AIRCRAFT LANDED IN MWH WITHOUT FURTHER PROBLEMS. NR 2 PROPELLER LEAKING OIL BECAUSE OF CUT PROP DOME O-RING. O-RING REPLACED I/A/W MAINT. MANUAL AND PROP OPS CHECKED GOOD. AIRCRAFT REMar 8, 1996 · N26877 · Swrngn SA227AC · Propeller Hub SectionSDR MALA964905Switch · dirtyFLT NR 3369 - DURING APPROACH TO DTW, THE NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. THE CREW RECYCLED THE GEAR TWICE AND THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLMar 8, 1996 · N421MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964902Frame · chafedDURING A SCHEDULED INSPECTION IN MSP, THE PASSENGER DOOR FORWARD SIDE FRAME WAS CHAFED THROUGH AT THE CENTER BAYONET AREA. REPAIRS WERE COMPLETED BY INSTALLING AN ELEVEN INCH DOUBLER IAW FAC SRM 52-90-10 PAGES 5-7 AS PER FAC LAR 96-MALA-043. (M)Mar 7, 1996 · N428MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964900Actuator · dirtyFLT NR 3346 - ON APPROACH TO CWA, THE RIGHT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR AND THE PROBLEM PERSISTED. THE CREW PERFORMED AN EMERGENCY EXTENSION AND ALL INDICATIONS WERE NORMAL. MAINTENANCE NOTED THAT THE EMERGENCY EXTENSMar 7, 1996 · N425MA · Swrngn SA227AC · Landing Gear ActuatorSDR MALA964901Corner · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LOWER FORWARD DOOR CORNER TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER IAW FAC SRM 51-00-00. (M)Mar 6, 1996 · N428MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964899Retract Mech · lack of lubeFLT NR 3271 - ON CLIMB-OUT FROM STC, THE NOSE GEAR BEGAN TO CYCLE AFTER THE GEAR WAS RETRACTED. THE CREW CYCLED THE GEAR UNTIL THE INTRANSIT LIGHT REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE WAS UNABLE TO DUPLIMar 6, 1996 · N60NE · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA4896Hyd Line · chafedFLT NR 3285 - AFTER DEPARTURE FROM MLI, BOTH HYDRAULIC PRESSURE CAUTION LIGHTS ILLUMINATED AND THE HYDRAULIC PRESSURE DROPPED TO ZERO. THE CREW ELECTED TO RETURN TO MLI AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED A HYDRAULIC PUMPMar 3, 1996 · N445MA · Swrngn SA227AC · Hydraulic System, MainSDR COMA9620004Nozzle · dirtyRT ENGINE WILL NOT ACHIEVE CHARTED TAKEOFF TORQUE. REPLACED THE ENGINE FUEL NOZZLES. POWER ASSURANCE RUNS NORMAL AND ACFT RETURNED TO SERVICE.Mar 3, 1996 · N704C · Swrngn SA227AC · Fuel Injector NozzleSDR SWIA95721Control Cable · failedON TAXI IN FELT POP IN RUDDER PEDALS. ON FURTHER INSPECTION, FOUND THE RUDDER PEDALS NO LONGER MOVE THE RUDDER. REPLACED RIGHT AFT RUDDER CABLE. ADJUSTED TENSION, CHECKED RIGGING. OPS CHECKS GOOD.Mar 2, 1996 · N685AV · Swrngn SA227AC · Rudder Control System
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